Active Control of a Multi-Stream Rectangular Supersonic Nozzle via Micro Jet Array
Author:
Affiliation:
1. Syracuse University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0851
Reference34 articles.
1. Simmons, R. J. “Design and control of a variable geometry turbofan with and independently modulated third stream,” Ph.D. thesis,The Ohio State University, 2009.
2. The nonaxisymmetric nozzle - It is for real<149>fighter aircraft performance viewpoint
3. An experimental and computational investigation of a translating throat single expansion-ramp nozzle
4. Cooled Cooling Air Systems for Turbine Thermal Management
5. Low-dimensional and data fusion techniques applied to a supersonic multistream single expansion ramp nozzle
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1. Schlieren-Based Analysis of Supersonic Multistream Control Using Data-Driven and Filtering Techniques;AIAA Journal;2024-09-02
2. Two-Dimensional Simulations of Multi-Stream Supersonic Jet Flow with Steady-Blowing Control;AIAA SCITECH 2024 Forum;2024-01-04
3. Experimental Efforts On the Control of a Multi-Stream Supersonic Rectangular Jet;AIAA SCITECH 2024 Forum;2024-01-04
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